EP3441156B1 - Methods for producing a matrix for pressure forming of workpieces - Google Patents
Methods for producing a matrix for pressure forming of workpieces Download PDFInfo
- Publication number
- EP3441156B1 EP3441156B1 EP17185483.9A EP17185483A EP3441156B1 EP 3441156 B1 EP3441156 B1 EP 3441156B1 EP 17185483 A EP17185483 A EP 17185483A EP 3441156 B1 EP3441156 B1 EP 3441156B1
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- EP
- European Patent Office
- Prior art keywords
- core
- die core
- die
- reinforcement body
- section
- Prior art date
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Links
- 238000000034 method Methods 0.000 title claims description 22
- 239000011159 matrix material Substances 0.000 title claims description 14
- 230000003014 reinforcing effect Effects 0.000 claims description 80
- 230000002787 reinforcement Effects 0.000 claims description 62
- 238000004519 manufacturing process Methods 0.000 claims description 27
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 26
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 26
- 229920003023 plastic Polymers 0.000 claims description 11
- 239000004033 plastic Substances 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 10
- 230000003247 decreasing effect Effects 0.000 claims description 7
- 239000000835 fiber Substances 0.000 claims description 7
- 230000002093 peripheral effect Effects 0.000 claims 5
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 9
- 230000008569 process Effects 0.000 description 7
- 239000012783 reinforcing fiber Substances 0.000 description 7
- 238000007493 shaping process Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 229920002492 poly(sulfone) Polymers 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 229920001169 thermoplastic Polymers 0.000 description 2
- 239000004416 thermosoftening plastic Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D37/00—Tools as parts of machines covered by this subclass
- B21D37/10—Die sets; Pillar guides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J13/00—Details of machines for forging, pressing, or hammering
- B21J13/02—Dies or mountings therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
- B21C25/02—Dies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
- B21C25/02—Dies
- B21C25/025—Selection of materials therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C3/00—Profiling tools for metal drawing; Combinations of dies and mandrels
- B21C3/02—Dies; Selection of material therefor; Cleaning thereof
- B21C3/04—Dies; Selection of material therefor; Cleaning thereof with non-adjustable section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/24—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass dies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/40—Plastics, e.g. foam or rubber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B15/00—Details of, or accessories for, presses; Auxiliary measures in connection with pressing
- B30B15/02—Dies; Inserts therefor; Mounting thereof; Moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B30—PRESSES
- B30B—PRESSES IN GENERAL
- B30B15/00—Details of, or accessories for, presses; Auxiliary measures in connection with pressing
- B30B15/02—Dies; Inserts therefor; Mounting thereof; Moulds
- B30B15/022—Moulds for compacting material in powder, granular of pasta form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P11/00—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for
- B23P11/02—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for by first expanding and then shrinking or vice versa, e.g. by using pressure fluids; by making force fits
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2101/00—Use of unspecified macromolecular compounds as moulding material
- B29K2101/12—Thermoplastic materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/757—Moulds, cores, dies
Definitions
- the invention relates to a method for producing a forming die for pressure forming of workpieces, in the context of which a die core of the forming die is provided on the outside with a core reinforcement in the form of a Arm michs stressess of fiber reinforced plastic such that the arranged on the die core Arm michs emotions the die core in the circumferential direction of the Die core around a Häddlingsachse of the die core, along which extends in the interior of the die core a workpiece holder of the die core, wherein the reinforcing body has a plastic matrix and a reinforcing fiber structure which is embedded in the plastic matrix and extending in the circumferential direction of the die core, wherein the reinforcing body Generation of a radial bias of the reinforcing body against the die core is applied to the die core, so that arranged on the die core Kernarmtechnik transversely to the Arbei tsschisachse is radially biased against the die core and wherein the Arm ists emotions is applied to generate a radial
- the workpiece to be formed is arranged in the workpiece holder in the interior of a die core.
- the wall of the workpiece holder of the die core is formed shaping and provided for this purpose, for example, with a shaping profile.
- the die core and the workpiece located inside the workpiece holder of the die core are moved relative to one another along a working movement axis of the die core. Due to the process, the workpiece exerts a large radial force on the die core transversely to the working movement axis.
- the die core In order to prevent undesirable deformation of the die core under the action of the radial force exerted by the workpiece, the die core is radially biased in the direction opposite to the working movement axis in the opposite direction of the radial force exerted by the workpiece.
- the die core is provided with a core reinforcement, which encloses the die core on its outer side in the circumferential direction about the working movement axis.
- the object of the present invention is to provide a comparison with the generic prior art simplified method for producing a forming die for pressure forming of workpieces.
- a core reinforcement which has a reinforcing body made of fiber-reinforced plastic which is radially prestressed against the die core.
- the reinforcing body comprises a plastic matrix and a reinforcing fiber structure embedded in the plastic matrix and extending in the circumferential direction of the die core about its working movement axis.
- a reinforcing body made of fiber-reinforced plastic is applied to the die core of the forming die as a core reinforcement to produce a radial prestressing of the reinforcing body against the die core on the outside of the die core.
- the reinforcing fiber structure of the reinforcing body may comprise short, long or continuous fibers.
- the plastic matrix of the reinforcing body is in particular a polymer matrix of thermosets or thermoplastics in question.
- the reinforcing body which consists of fiber-reinforced plastic, is characterized by a high load carrying capacity and at the same time low volume and low mass out. Due to the small size, the forming die produced according to the claim can be accommodated on a forming machine to save space. The reduced mass of the forming die, for example, when handling them as part of a tool change of considerable advantage. In addition, such forming dies are cheaper than conventional forming dies for pressure forming of workpieces.
- fiber-reinforced plastic is applied in the uncured state on the outside of the die core to create a radially biased against the die core Arm ists stressess, wherein the die core at the time of application of the fiber reinforced plastic has a mounting core cross-section which is smaller as a utility core cross-section present in a use state of the die core.
- the reduced cross-section of the die core for the assembly is increased to the cross-section which the die core has during workpiece reshaping.
- Connected to the cross-sectional enlargement of the die core occurring when the reinforcing body has hardened is the generation of a radial prestressing of the hardened reinforcing body against the die core.
- the reinforcing body before application to the die core as a cured hollow body.
- the hardened reinforcing body has a core receptacle for the die core of the forming die according to the invention.
- a core receiving axis of the reinforcing body extends in the installed position of the die core in the interior of the reinforcing body along the working movement axis of the die core.
- the core receptacle of the reinforcing body has a core receiving opening at least on one side. In a mounting initial state of the reinforcing body whose core receptacle has an output core receiving cross-section.
- the core receiving cross section is increased relative to the starting core receiving cross section in order to produce a readiness for assembly of the reinforcing body and of the die core.
- the reinforcing body and the die core are moved relative to each other along the core receiving axis of the reinforcing body or along the Häzingsache of the die core. If the reinforcing body is arranged on the outside of the die core in the desired position after the joining process, finally the core receiving cross section of the reinforcing body is reduced. As a result, a radial prestressing of the reinforcing body is produced against the die core.
- claim 3 for producing a readiness for assembly of the reinforcing body and the die core of the core receiving cross section of the reinforcing body relative to the output core receiving cross-section enlarged and also reduces the core cross-section of the die core relative to the utility core cross-section. If the reinforcing body is arranged in the desired position on the outside of the die core after the joining process, finally the core receiving cross section of the reinforcing body is reduced and, in addition, the core cross section of the die core is enlarged. As a result, a radial prestressing of the reinforcing body is produced against the die core.
- the reinforcement body of fiber-reinforced plastic is applied directly to the die core in a preferred embodiment of the manufacturing method according to the invention according to claims 1 and 2.
- the reinforcement body of fiber-reinforced plastic is applied directly to the die core in a preferred embodiment of the manufacturing method according to the invention according to claims 1 and 2.
- the die core is lengthened relative to its use state along the working movement axis of the die core, preferably elastically elongated (claim 5) and / or the temperature of the die core is changed with respect to the temperature in the use state of the die core, reduced at corresponding temperature behavior of the material of the die core (claim 6).
- the temperature of the reinforcing body present as a cured hollow body is changed in relation to the temperature at assembly initial state of the reinforcing body, depending on the temperature behavior of the Armier stresses increased or decreased (claim 7).
- Claim 8 relates to a manufacturing method according to the invention, in the context of which a reinforcing body made of carbon fiber reinforced plastic (CFRP) is applied to generate a radial bias of the reinforcing body against the die core on the die core.
- CFRP carbon fiber reinforced plastic
- the reinforcement fiber structure extending in the circumferential direction of the die core of a reinforcing body made of carbon fiber reinforced plastic applied to the die core permits, in a particularly lightweight construction, a particularly effective prestressing of the reinforcing body against the die core of the forming die according to the invention.
- a forming die 1 for pressure forming in the present case for the axial forming of workpieces, comprises a die core 2 made of steel and a reinforcing body 3 made of carbon fiber-reinforced plastic (CFRP).
- the die core 2 is hollow cylindrical and has a workpiece holder 4 in its interior.
- the workpiece holder 4 extends along a working movement axis 5 of the die core 2, which forms the symmetry axis of the die core 2.
- An axially parallel inner wall 6 of the die core 2 delimiting the workpiece holder 4 is in the usual way with a shaping profile (not shown in FIGS. 1a, 1b) Mistake.
- An axially parallel outer wall of the die core 2 defines a core cross section QM of the die core 2.
- the workpiece arranged in the interior of the workpiece holder 4 and the forming die 1 are moved as usual along the working movement axis 5 relative to one another.
- the workpiece is claimed by the shaping profile of the die core 2 beyond the yield point and thereby formed.
- the workpiece exerts a large radial force on the die core 2 during its deformation.
- the effective direction of the force exerted by the workpiece on the die core 2 radial force is in the FIGS. 1a, 1b illustrated by arrows.
- the die core 2 is not undesirably deformed under the action of the radial force exerted by the workpiece, and the reinforcing body 3 is provided to increase the load bearing capacity of the die core 2.
- the reinforcing body 3 is formed in the illustrated example in the manner of a CFRP tube with a wound continuous filament structure.
- the die core 2 is arranged in a core receptacle 7 of the reinforcing body 3.
- a core receiving axis 8 of the reinforcing body 3 coincides with the working movement axis 5 of the die core 2 in the installed position of the die core 2 in the core receptacle 7 of the reinforcing body 3.
- An axially parallel inner wall of the core receptacle 7 delimits a core receiving cross section QA of the reinforcing body 3.
- FIGS. 1a, 1b is the forming die 1 and with this the die core 2 and the Arm ists stresses 3 in use, in which with the forming die 1, a forming process can be performed.
- the reinforcing body 3 is radially biased against the die core 2 counter to the direction of the radial force exerted on the die core 2 by the workpiece during the forming process.
- the die core 2 has a utility core cross section
- the core receptacle 7 of the reinforcing body 3 has a utility core receiving cross section.
- the die core 2 is elastically elongated along the working movement axis 5 (method step (1) in FIG. 2 ).
- the die core 2 receives, as the core cross-section QM, a mounting core cross section which is smaller than the useful core cross section.
- fiber-reinforced plastic in the wet state is applied to the outside of the cross-section reduced die core 2 in such a way that an in FIG. 2 shown in a highly schematically illustrated reinforcing fiber structure 9 of the fiber-reinforced plastic with continuous fibers of carbon in the circumferential direction of the die core 2 about the working movement axis 5 (method step (2) in FIG FIG. 2 ).
- the reinforcing fiber structure 9 with carbon continuous fibers is embedded in a thermoplastic matrix (for example polysulfone / PSU) of the fiber-reinforced plastic.
- the core receptacle 7 In the interior of the hardened reinforcing body 3, where the mandrel 10 was previously arranged, the core receptacle 7 is formed, which has a core receiving opening 1 on both sides along the core receiving axis 8.
- the core receptacle 7 of the Arm ists stressess 3 in this phase of the illustrated manufacturing method has an output core receiving cross section.
- the temperature of the reinforcing body 3 is changed, in the illustrated example, the reinforcing body 3 is cooled. Due to the corresponding temperature behavior of the carbon fiber reinforced plastic used here, the cooling leads to a widening of the reinforcing body 3 and, associated therewith, to an enlargement of the core receiving cross section QA of the reinforcing body 3 with respect to the starting core receiving cross section (step (3) in FIG. 3 ). Thus, the reinforcing body 3 is ready for assembly.
- the die core 2 is cooled starting from its use state.
- the core cross section QM of the die core 2 is reduced relative to the use core cross section (step (4) in FIG. 3 ).
- the die core 2 is ready to install.
- the core cross-section QM of the ready-to-install die core 2 is smaller than the core receiving cross-section QA of the ready-to-fit Arm ists stressess 2, wherein the core cross-section QM of the ready Matrizenenkerns 2 in the vertical projection on the core receiving cross section QA of the ready Arm ists stressess 3 within the core receiving cross section QA of the ready-Armings stressess 3.
- the reinforcing body 3 and the die core 2 are joined by inserting the ready-to-install die core 2 through one of the core receiving openings 11 of the reinforcing body 3 along the core receiving axis 8 into the core seat 7 of the reinforcing body 3 (operation (5) in FIG. 3 ).
- the unit of reinforcing body 3 and die core 2 is heated (step (6) in FIG. 3 ). Due to the heating, the core cross section QM of the die core 2 increases, while the core receiving cross section QA of the reinforcing body 3 decreases. As a result of the enlargement of the core cross section QM of the die core 2 with simultaneous reduction of the core receiving cross section QA of the reinforcing body 3, the reinforcing body 3 is prestressed radially against the female body 2. The production of the forming die 1 is completed.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Robotics (AREA)
- Moulding By Coating Moulds (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Mounting, Exchange, And Manufacturing Of Dies (AREA)
Description
Die Erfindung betrifft ein Verfahren zur Herstellung einer Umformmatrize zum Druckumformen von Werkstücken, im Rahmen dessen ein Matrizenkern der Umformmatrize an der Außenseite mit einer Kernarmierung in Form eines Armierungskörpers aus faserverstärktem Kunststoff versehen wird derart, dass der auf dem Matrizenkern angeordnete Armierungskörper den Matrizenkern in Umfangsrichtung des Matrizenkerns um eine Arbeitsbewegungsachse des Matrizenkerns umschließt, entlang derer sich im Innern des Matrizenkerns eine Werkstückaufnahme des Matrizenkerns erstreckt, wobei der Armierungskörper eine Kunststoffmatrix und eine Verstärkungsfaserstruktur aufweist, die in die Kunststoffmatrix eingebettet ist und sich in der Umfangsrichtung des Matrizenkerns erstreckt, wobei der Armierungskörper unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf den Matrizenkern aufgebracht wird, so dass die auf dem Matrizenkern angeordnete Kernarmierung quer zu der Arbeitsbewegungsachse gegen den Matrizenkern radial vorgespannt ist und wobei der Armierungskörper unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf den Matrizenkern aufgebracht wird, indem ein sich senkrecht zu der Arbeitsbewegungsachse erstreckender Kernquerschnitt des Matrizenkerns gegenüber einem bei einem Gebrauchszustand des Matrizenkerns vorliegenden Gebrauchs-Kernquerschnitt auf einen Montage-Kernquerschnitt verkleinert wird.The invention relates to a method for producing a forming die for pressure forming of workpieces, in the context of which a die core of the forming die is provided on the outside with a core reinforcement in the form of a Armierungskörpers of fiber reinforced plastic such that the arranged on the die core Armierungskörper the die core in the circumferential direction of the Die core around a Arbeitsbewegungsachse of the die core, along which extends in the interior of the die core a workpiece holder of the die core, wherein the reinforcing body has a plastic matrix and a reinforcing fiber structure which is embedded in the plastic matrix and extending in the circumferential direction of the die core, wherein the reinforcing body Generation of a radial bias of the reinforcing body against the die core is applied to the die core, so that arranged on the die core Kernarmierung transversely to the Arbei tsbewegungsachse is radially biased against the die core and wherein the Armierungskörper is applied to generate a radial bias of the Armierungskörpers against the die core on the die core by a perpendicular to the Arbeitsbewegungsachse extending core cross-section of the die core against a present in a state of use of the die core utility core cross section a mounting core cross-section is reduced.
Die Erfindung betrifft des Weiteren ein Verfahren zur Herstellung einer Umformmatrize zum Druckumformen von Werkstücken, im Rahmen dessen ein Matrizenkern der Umformmatrize an der Außenseite mit einer Kernarmierung in Form eines Armierungskörpers aus faserverstärktem Kunststoff versehen wird derart, dass der auf dem Matrizenkern angeordnete Armierungskörper den Matrizenkern in Umfangsrichtung des Matrizenkerns um eine Arbeitsbewegungsachse des Matrizenkerns umschließt, entlang derer sich im Innern des Matrizenkerns eine Werkstückaufnahme des Matrizenkerns erstreckt, wobei der Armierungskörper eine Kunststoffmatrix und eine Verstärkungsfaserstruktur aufweist, die in die Kunststoffmatrix eingebettet ist und sich in der Umfangsrichtung des Matrizenkerns erstreckt, wobei der Armierungskörper unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf den Matrizenkern aufgebracht wird, so dass die auf dem Matrizenkern angeordnete Kernarmierung quer zu der Arbeitsbewegungsachse gegen den Matrizenkern radial vorgespannt ist und wobei der Armierungskörper unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf den Matrizenkern aufgebracht wird,
- indem der Armierungskörper als ausgehärteter Hohlkörper hergestellt wird, der in seinem Innern für den Matrizenkern eine Kernaufnahme aufweist, wobei die Kernaufnahme des Armierungskörpers eine sich bei Einbaulage des Matrizenkerns längs der Arbeitsbewegungsachse des Matrizenkerns erstreckende Kernaufnahmeachse aufweist, wobei die Kernaufnahme des Armierungskörpers längs der Kernaufnahmeachse wenigstens einseitig eine Kernaufnahmeöffnung aufweist und wobei die Kernaufnahme des Armierungskörpers in einem Montage-Ausgangszustand des Armierungskörpers einen sich senkrecht zu der Kernaufnahmeachse erstreckenden Ausgangs-Kernaufnahmequerschnitt besitzt,
- indem eine Montagebereitschaft des Armierungskörpers und des Matrizenkerns hergestellt wird und
- indem der montagebereite Armierungskörper und der montagebereite Matrizenkern gefügt werden, wobei der montagebereite Matrizenkern durch die Kernaufnahmeöffnung des montagebereiten Armierungskörpers längs der Kernaufnahmeachse in die Kernaufnahme des montagebereiten Armierungskörpers eingeführt und dadurch der Armierungskörper auf der Außenseite des Matrizenkerns angeordnet wird.
- in that the reinforcing body is produced as a hardened hollow body which has a core receptacle in its interior for the die core, the core receptacle of the reinforcing body having a core receiving axis extending along the working movement axis of the die core in the installed position of the die core, the core receptacle of the reinforcing body being at least one side along the core receiving axis has a core receiving opening and wherein the core receptacle of the reinforcing body has an output core receiving cross section extending perpendicularly to the core receiving axis in a mounting initial state of the reinforcing body,
- by an assembly readiness of the Armierungskörpers and the die core is made and
- by fitting the ready-to-install armoring body and the ready-to-install die core, the ready-to-install die core being inserted through the core receiving opening of the ready-to-use arming body along the core receiving axis into the core receptacle of the ready-to-mount armoring body, thereby placing the armor body on the outside of the die core.
Beim Druckumformen von Werkstücken mittels einer Umformmatrize ist das umzuformende Werkstück in der Werkstückaufnahme im Innern eines Matrizenkerns angeordnet. Die Wand der Werkstückaufnahme des Matrizenkerns ist formgebend ausgebildet und zu diesem Zweck beispielsweise mit einem formgebenden Profil versehen. Während des Umformprozesses werden der Matrizenkern und das im Innern der Werkstückaufnahme des Matrizenkerns angeordnete Werkstück längs einer Arbeitsbewegungsachse des Matrizenkerns relativ zueinander bewegt. Prozessbedingt übt das Werkstück dabei quer zu der Arbeitsbewegungsachse eine große Radialkraft auf den Matrizenkern aus. Um eine unerwünschte Verformung des Matrizenkerns unter der Wirkung der von dem Werkstück ausgeübten Radialkraft zu verhindern, ist der Matrizenkern in Gegenrichtung der von dem Werkstück ausgeübten Radialkraft in Richtung auf die Arbeitsbewegungsachse radial vorgespannt. Zur Erhöhung seiner Lastaufnahmefähigkeit ist der Matrizenkern mit einer Kernarmierung versehen, welche den Matrizenkern an dessen Außenseite in Umfangsrichtung um die Arbeitsbewegungsachse umschließt.When pressure forming of workpieces by means of a forming die, the workpiece to be formed is arranged in the workpiece holder in the interior of a die core. The wall of the workpiece holder of the die core is formed shaping and provided for this purpose, for example, with a shaping profile. During the forming process, the die core and the workpiece located inside the workpiece holder of the die core are moved relative to one another along a working movement axis of the die core. Due to the process, the workpiece exerts a large radial force on the die core transversely to the working movement axis. In order to prevent undesirable deformation of the die core under the action of the radial force exerted by the workpiece, the die core is radially biased in the direction opposite to the working movement axis in the opposite direction of the radial force exerted by the workpiece. To increase its load-bearing capacity, the die core is provided with a core reinforcement, which encloses the die core on its outer side in the circumferential direction about the working movement axis.
Gattungsgemäßer Stand der Technik ist offenbart in
Weiterer Stand der Technik ist bekannt aus
Die Aufgabe der vorliegenden Erfindung besteht darin, ein gegenüber dem gattungsgemäßen Stand der Technik vereinfachtes Verfahren zur Herstellung einer Umformmatrize zum Druckumformen von Werkstücken bereitzustellen.The object of the present invention is to provide a comparison with the generic prior art simplified method for producing a forming die for pressure forming of workpieces.
Erfindungsgemäß gelöst wird diese Aufgabe durch das Verfahren gemäß Patentanspruch 1 und durch das Verfahren gemäß Patentanspruch 2.This object is achieved according to the invention by the method according to
Für den Matrizenkern der anspruchsgemäß hergestellten Umformmatrize ist eine Kernarmierung vorgesehen, die einen gegen den Matrizenkern radial vorgespannten Armierungskörper aus faserverstärktem Kunststoff aufweist. Der Armierungskörper umfasst eine Kunststoffmatrix sowie eine in die Kunststoffmatrix eingebettete und sich in der Umfangsrichtung des Matrizenkerns um dessen Arbeitsbewegungsachse erstreckende Verstärkungsfaserstruktur. Im Rahmen der anspruchsgemäßen Herstellungsverfahren wird auf den Matrizenkern der Umformmatrize als Kernarmierung ein Armierungskörper aus faserverstärktem Kunststoff unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf die Außenseite des Matrizenkerns aufgebracht.For the die core of the forming die produced according to the claims, a core reinforcement is provided which has a reinforcing body made of fiber-reinforced plastic which is radially prestressed against the die core. The reinforcing body comprises a plastic matrix and a reinforcing fiber structure embedded in the plastic matrix and extending in the circumferential direction of the die core about its working movement axis. In the context of the claimed manufacturing process, a reinforcing body made of fiber-reinforced plastic is applied to the die core of the forming die as a core reinforcement to produce a radial prestressing of the reinforcing body against the die core on the outside of the die core.
Die Verstärkungsfaserstruktur des Armierungskörpers kann Kurz-, Lang- oder Endlosfasern aufweisen. Als Kunststoffmatrix des Armierungskörpers kommt insbesondere eine polymere Matrix aus Duromeren oder Thermoplasten infrage.The reinforcing fiber structure of the reinforcing body may comprise short, long or continuous fibers. The plastic matrix of the reinforcing body is in particular a polymer matrix of thermosets or thermoplastics in question.
Der aus faserverstärktem Kunststoff bestehende Armierungskörper zeichnet sich durch eine große Lastaufnahmefähigkeit bei gleichzeitig geringem Volumen und geringer Masse aus. Aufgrund der geringen Baugröße lässt sich die anspruchsgemäß hergestellte Umformmatrize an einer Umformmaschine platzsparend unterbringen. Die reduzierte Masse der Umformmatrize ist beispielsweise bei deren Handling im Rahmen eines Werkzeugwechsels von erheblichem Vorteil. Zudem sind derartige Umformmatrizen kostengünstiger als herkömmliche Umformmatrizen zum Druckumformen von Werkstücken.The reinforcing body, which consists of fiber-reinforced plastic, is characterized by a high load carrying capacity and at the same time low volume and low mass out. Due to the small size, the forming die produced according to the claim can be accommodated on a forming machine to save space. The reduced mass of the forming die, for example, when handling them as part of a tool change of considerable advantage. In addition, such forming dies are cheaper than conventional forming dies for pressure forming of workpieces.
Im Rahmen des erfindungsgemäßen Herstellungsverfahrens gemäß Patentanspruch 1 wird zur Erstellung eines gegen den Matrizenkern radial vorgespannten Armierungskörpers faserverstärkter Kunststoff im nicht ausgehärteten Zustand auf die Außenseite des Matrizenkerns aufgebracht, wobei der Matrizenkern zum Zeitpunkt des Aufbringens des faserverstärkten Kunststoffs einen Montage-Kernquerschnitt aufweist, der kleiner ist als ein bei einem Gebrauchszustand des Matrizenkerns vorliegender Gebrauchs-Kernquerschnitt. Nach dem Aushärten des im nassen Zustand aufgebrachten faserverstärkten Kunststoffs wird der für die Montage reduzierte Querschnitt des Matrizenkerns auf denjenigen Querschnitt vergrößert, welchen der Matrizenkern bei der Werkstückumformung aufweist. Mit der bei ausgehärtetem Armierungskörper erfolgenden Querschnittsvergrößerung des Matrizenkerns verbunden ist die Erzeugung einer radialen Vorspannung des ausgehärteten Armierungskörpers gegen den Matrizenkern.In the context of the inventive manufacturing method according to claim 1 fiber-reinforced plastic is applied in the uncured state on the outside of the die core to create a radially biased against the die core Armierungskörpers, wherein the die core at the time of application of the fiber reinforced plastic has a mounting core cross-section which is smaller as a utility core cross-section present in a use state of the die core. After curing of the fiber-reinforced plastic applied in the wet state, the reduced cross-section of the die core for the assembly is increased to the cross-section which the die core has during workpiece reshaping. Connected to the cross-sectional enlargement of the die core occurring when the reinforcing body has hardened is the generation of a radial prestressing of the hardened reinforcing body against the die core.
Alternativ liegt im Rahmen des Herstellungsverfahrens gemäß Patentanspruch 2 der Armierungskörper vor dem Aufbringen auf den Matrizenkern als ausgehärteter Hohlkörper vor. In seinem Innern weist der ausgehärtete Armierungskörper eine Kernaufnahme für den Matrizenkern der erfindungsgemäßen Umformmatrize auf. Eine Kernaufnahmeachse des Armierungskörpers erstreckt sich bei Einbaulage des Matrizenkerns im Innern des Armierungskörpers längs der Arbeitsbewegungsachse des Matrizenkerns. Längs der Kernaufnahmeachse weist die Kernaufnahme des Armierungskörpers wenigstens einseitig eine Kernaufnahmeöffnung auf. In einem Montage-Ausgangszustand des Armierungskörpers besitzt dessen Kernaufnahme einen Ausgangs-Kernaufnahmequerschnitt. Erfindungsgemäß wird zur Herstellung einer Montagebereitschaft des Armierungskörpers und des Matrizenkerns der Kernaufnahmequerschnitt gegenüber dem Ausgangs-Kernaufnahmequerschnitt vergrößert. Dadurch wird erreicht, dass der Kernaufnahmequerschnitt des montagebereiten Armierungskörpers derart bemessen ist, dass der Kernquerschnitt des montagebereiten Matrizenkerns in der senkrechten Projektion auf den Kernaufnahmequerschnitt innerhalb des Kernaufnahmequerschnitts liegt und folglich der Matrizenkern zum Aufbringen des Armierungskörpers in die Kernaufnahme des Armierungskörpers eingeführt werden kann. Nach der Herstellung der Montagebereitschaft des Armierungskörpers und des Matrizenkerns werden der montagebereite Armierungskörper und der montagebereite Matrizenkern entsprechend gefügt. Dabei werden der Armierungskörper und der Matrizenkern relativ zueinander längs der Kernaufnahmeachse des Armierungskörpers beziehungsweise längs der Arbeitsbewegungsache des Matrizenkerns bewegt. Ist der Armierungskörper nach dem Fügevorgang auf der Außenseite des Matrizenkerns in der Sollposition angeordnet, wird schließlich der Kernaufnahmequerschnitt des Armierungskörpers verkleinert. Dadurch wird eine radiale Vorspannung des Armierungskörpers gegen den Matrizenkern erzeugt.Alternatively, in the context of the manufacturing method according to
Besondere Ausführungsarten der erfindungsgemäßen Herstellungsverfahren nach den Patentansprüchen 1 und 2 ergeben sich aus den abhängigen Patentansprüchen 3 bis 8.Particular embodiments of the manufacturing method according to the invention according to
In Weiterbildung des erfindungsgemäßen Verfahrens nach Patentanspruch 2 wird ausweislich Patentanspruch 3 zur Herstellung einer Montagebereitschaft des Armierungskörpers und des Matrizenkerns der Kernaufnahmequerschnitt des Armierungskörpers gegenüber dem Ausgangs-Kernaufnahmequerschnitt vergrößert und außerdem der Kernquerschnitt des Matrizenkerns gegenüber dem Gebrauchs-Kernquerschnitt verkleinert. Ist der Armierungskörper nach dem Fügevorgang auf der Außenseite des Matrizenkerns in der Sollposition angeordnet, wird schließlich der Kernaufnahmequerschnitt des Armierungskörpers verkleinert und außerdem wird der Kernquerschnitt des Matrizenkerns vergrö-ßert. Dadurch wird eine radiale Vorspannung des Armierungskörpers gegen den Matrizenkern erzeugt.In a further development of the method according to
Gemäß Patentanspruch 4 wird in bevorzugter Ausgestaltung der erfindungsgemäßen Herstellungsverfahren nach den Patentansprüchen 1 und 2 der Armierungskörper aus faserverstärktem Kunststoff unmittelbar auf den Matrizenkern aufgebracht. Infolgedessen ergibt sich als Umformmatrize eine besonders kompakt bauende Einheit aus Matrizenkern und Armierungskörper.According to
Sowohl im Rahmen des erfindungsgemäßen Herstellungsverfahrens gemäß Patentanspruch 1 als auch im Rahmen des erfindungsgemäßen Herstellungsverfahrens gemäß Patentanspruch 3 bedarf es einer Verkleinerung des Kernquerschnitts des Matrizenkerns gegenüber dem Gebrauchs-Kernquerschnitt. In vorteilhafter Ausgestaltung der erfindungsgemäßen Herstellungsverfahren wird zu diesem Zweck der Matrizenkern gegenüber seinem Gebrauchszustand längs der Arbeitsbewegungsachse des Matrizenkerns gelängt, vorzugsweise elastisch gelängt (Patentanspruch 5) und/oder die Temperatur des Matrizenkerns wird gegenüber der Temperatur bei Gebrauchszustand des Matrizenkerns verändert, bei entsprechendem Temperaturverhalten des Werkstoffs des Matrizenkerns reduziert (Patentanspruch 6).Both in the context of the inventive manufacturing method according to
Zur Vergrößerung des Kernaufnahmequerschnitts des Armierungskörpers gegenüber dem Ausgangs-Kernaufnahmequerschnitt im Rahmen des erfindungsgemäßen Herstellungsverfahrens gemäß Patentanspruch 2 wird in weiterer vorteilhafter Ausgestaltung des erfindungsgemäßen Herstellungsverfahrens die Temperatur des als ausgehärteter Hohlkörper vorliegenden Armierungskörpers gegenüber der Temperatur bei Montage-Ausgangszustand des Armierungskörpers verändert, je nach Temperaturverhalten des Armierungskörpers erhöht oder gesenkt (Patentanspruch 7).To increase the core receiving cross section of the reinforcing body relative to the starting core receiving cross section in the manufacturing process according to
Im Rahmen der erfindungsgemäßen Herstellungsverfahren können für den Armierungskörper der erfindungsgemäßen Umformmatrize verschiedenartige faserverstärkte Kunststoffe verwendet werden. Patentanspruch 8 betrifft ein erfindungsgemäßes Herstellungsverfahren, im Rahmen dessen ein Armierungskörper aus kohlenstofffaserverstärktem Kunststoff (CFK) unter Erzeugung einer radialen Vorspannung des Armierungskörpers gegen den Matrizenkern auf den Matrizenkern aufgebracht wird. Kohlenstofffaserverstärkte Kunststoffe zeichnen sich durch eine besonders hohe Zugfestigkeit bei geringer Dichte aus. Die sich in der Umfangsrichtung des Matrizenkerns erstreckende Verstärkungsfaserstruktur eines auf den Matrizenkern aufgebrachten Armierungskörpers aus kohlenstofffaserverstärktem Kunststoff gestattet bei besonders leichter Bauweise eine besonders wirksame Vorspannung des Armierungskörpers gegen den Matrizenkern der erfindungsgemäßen Umformmatrize.In the context of the production method according to the invention, various fiber-reinforced plastics can be used for the reinforcing body of the forming die according to the invention.
Werden im Rahmen des erfindungsgemäßen Herstellungsverfahrens gemäß Patentanspruch 3 ein Armierungskörper aus kohlenstofffaserverstärktem Kunststoff (negativer Wärmeausdehnungskoeffizient) und ein Matrizenkern aus einem Material mit einem positiven Wärmeausdehnungskoeffizienten, beispielsweise aus Stahl, gefügt und werden zur Herstellung der Montagebereitschaft des Armierungskörpers und des Matrizenkerns und/oder zur Erzeugung der radialen Vorspannung des Armierungskörpers gegen den Matrizenkern die Temperaturen des Armierungskörpers und des Matrizenkerns verändert, so kann jeweils eine gleichsinnige Temperaturänderung der beiden Teile der erfindungsgemäßen Umformmatrize vorgenommen werden. Aufgrund des Temperaturverhaltens der Werkstoffe des Armierungskörpers und des Matrizenkerns sind die beiderseitigen Temperaturen zur Herstellung der Montagebereitschaft zu senken und zur Erzeugung der radialen Vorspannung des Armierungskörpers gegen den Matrizenkern zu erhöhen.Are in the context of the manufacturing method according to
Nachfolgend wird die Erfindung anhand beispielhafter schematischer Darstellungen näher erläutert. Es zeigen:
- Figuren 1a, 1b
- Schnittdarstellungen einer Umformmatrize zum Druckumformen von Werkstücken, mit einem Matrizenkern und einer Kernarmierung,
Figur 2- den Ablauf einer ersten Variante eines Verfahrens zur Herstellung der Umformmatrize gemäß den Figuren la, 1b und
Figur 3- den Ablauf einer zweiten Variante des Verfahrens zur Herstellung der Umformmatrize gemäß den Figuren la, 1b.
- FIGS. 1a, 1b
- Sectional views of a forming die for pressure forming of workpieces, with a die core and a core reinforcement,
- FIG. 2
- the sequence of a first variant of a method for producing the forming die according to the figures la, 1b and
- FIG. 3
- the sequence of a second variant of the method for producing the forming die according to the figures la, 1b.
Gemäß den Figuren la, 1b umfasst eine Umformmatrize 1 zum Druckumformen, vorliegend zum Axialformen von Werkstücken einen Matrizenkern 2 aus Stahl sowie einen Armierungskörper 3 aus kohlenstofffaserfaserverstärktem Kunststoff (CFK). Der Matrizenkern 2 ist hohlzylindrisch ausgebildet und weist in seinem Innern eine Werkstückaufnahme 4 auf. Die Werkstückaufnahme 4 erstreckt sich längs einer Arbeitsbewegungsachse 5 des Matrizenkerns 2, welche die Symmetrieachse des Matrizenkerns 2 bildet. Eine die Werkstückaufnahme 4 begrenzende achsparallele Innenwand 6 des Matrizenkerns 2 ist in gewohnter Weise mit einem in den Figuren la, 1b nicht gezeigten formgebenden Profil versehen. Eine achsparallele Außenwand des Matrizenkerns 2 begrenzt einen Kernquerschnitt QM des Matrizenkerns 2.According to FIGS. 1a, 1b, a forming
Zum Druckumformen von Werkstücken, beispielsweise von Rohren, mittels der Umformmatrize 1 werden das im Innern der Werkstückaufnahme 4 angeordnete Werkstück und die Umformmatrize 1 wie üblich längs der Arbeitsbewegungsachse 5 relativ zueinander bewegt. Dabei wird das Werkstück durch das formgebende Profil des Matrizenkerns 2 über die Fließgrenze hinaus beansprucht und dadurch umgeformt.For pressure forming of workpieces, for example pipes, by means of the forming
Prozessbedingt übt das Werkstück bei seiner Umformung eine große Radialkraft auf den Matrizenkern 2 aus. Die Wirkrichtung der von dem Werkstück auf den Matrizenkern 2 ausgeübten Radialkraft ist in den
Damit der Matrizenkern 2 unter der Wirkung der von dem Werkstück ausgeübten Radialkraft nicht in unerwünschter Weise verformt wird und zur Erhöhung der Lastaufnahmefähigkeit des Matrizenkerns 2 ist der Armierungskörper 3 vorgesehen. Der Armierungskörper 3 ist in dem dargestellten Beispielsfall nach Art eines CFK-Rohrs mit einer gewickelten Endlosfaserstruktur ausgebildet.Thus, the
Der Matrizenkern 2 ist in einer Kernaufnahme 7 des Armierungskörpers 3 angeordnet. Eine Kernaufnahmeachse 8 des Armierungskörpers 3 fällt bei Einbaulage des Matrizenkerns 2 in der Kernaufnahme 7 des Armierungskörpers 3 mit der Arbeitsbewegungsachse 5 des Matrizenkerns 2 zusammen. Eine achsparallele Innenwand der Kernaufnahme 7 begrenzt einen Kernaufnahmequerschnitt QA des Armierungskörpers 3.The
In den
Zwei Möglichkeiten zur Herstellung der Umformmatrize 1 sind in den
Gemäß
Anschließend wird auf die Außenseite des querschnittsreduzierten Matrizenkerns 2 faserverstärkter Kunststoff im nassen Zustand derart aufgebracht, dass sich eine in
Bei nach wie vor querschnittsreduziertem Matrizenkern 2 wird der anfangs nasse faserverstärkte Kunststoff getempert und dadurch ausgehärtet (Verfahrensschritt (3) in
Abweichend von der in
Nachdem der Armierungskörper 3 als ausgehärteter Hohlkörper bereitgestellt worden ist, wird die Temperatur des Armierungskörpers 3 geändert, in dem dargestellten Beispielsfall wird der Armierungskörper 3 abgekühlt. Aufgrund des entsprechenden Temperaturverhaltens des vorliegend eingesetzten kohlenstofffaserverstärkten Kunststoffs führt die Abkühlung zu einer Aufweitung des Armierungskörpers 3 und damit verbunden zu einer Vergrößerung des Kernaufnahmequerschnitts QA des Armierungskörpers 3 gegenüber dem Ausgangs-Kernaufnahmequerschnitt (Arbeitsschritt (3) in
Zur Herstellung der Montagebereitschaft des Matrizenkerns 2 wird der Matrizenkern 2 ausgehend von seinem Gebrauchszustand abgekühlt. Dadurch wird der Kernquerschnitt QM des Matrizenkerns 2 gegenüber dem Gebrauchs-Kernquerschnitt verkleinert (Arbeitsschritt (4) in
Der Kernquerschnitt QM des montagebereiten Matrizenkerns 2 ist kleiner als der Kernaufnahmequerschnitt QA des montagebereiten Armierungskörpers 2, wobei der Kernquerschnitt QM des montagebereiten Matrizenkerns 2 in der senkrechten Projektion auf den Kernaufnahmequerschnitt QA des montagebereiten Armierungskörpers 3 innerhalb des Kernaufnahmequerschnitts QA des montagebereiten Armierungskörpers 3 liegt.The core cross-section QM of the ready-to-install
Nach der Herstellung der Montagebereitschaft des Armierungskörpers 3 und des Matrizenkerns 2 werden der Armierungskörper 3 und der Matrizenkern 2 gefügt, indem der montagebereite Matrizenkern 2 durch eine der Kernaufnahmeöffnungen 11 des Armierungskörpers 3 längs der Kernaufnahmeachse 8 in die Kernaufnahme 7 des Armierungskörpers 3 eingeschoben wird (Arbeitsschritt (5) in
Nachdem der Matrizenkern 2 seine Sollposition im Innern des Armierungskörpers 3 eingenommen hat, wird die Einheit aus Armierungskörper 3 und Matrizenkern 2 erwärmt (Arbeitsschritt (6) in
Claims (8)
- Method for producing a forming die (1) for pressure-forming workpieces, in which a die core (2) of the forming die (1) is provided at the outer side with a core reinforcement in the form of a reinforcement body (3) made of a fibre-reinforced plastics material in such a manner that the reinforcement body (3) arranged on the die core (2) surrounds the die core (2) in a peripheral direction of the die core (2) around a working movement axis (5) of the die core (2), along which working movement axis a workpiece receiving member (4) of the die core (2) extends inside the die core (2), wherein the reinforcement body (3) comprises a plastics matrix and a reinforcing fibre structure (9) which is embedded in the plastics matrix and which extends in the peripheral direction of the die core (2) wherein the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2) such that the core reinforcement which is arranged on the die core (2) is radially pretensioned transversely to the working movement axis (5) against the die core (2), and wherein the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2) by a core cross-section (QM) of the die core (2) which extends perpendicularly to the working movement axis (5) being decreased to an assembly core cross-section with respect to a core cross-section for use which is present in a state for use of the die core (2),
characterised in that the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2)• by the fibre-reinforced plastics material in the non-hardened state being applied to the outer side of the die core (2) which has the assembly core cross-section in such a manner that the reinforcing fibre structure (9) of the fibre-reinforced plastics material extends in the peripheral direction of the die core (2) which has the assembly core cross-section and• by the core cross-section (QM) of the die core (2) being increased to the core cross-section for use after the hardening of the fibre-reinforced plastics material applied to the outer side of the die core (2). - Method for producing a forming die (1) for pressure-forming workpieces, in which a die core (2) of the forming die (1) is provided at the outer side with a core reinforcement in the form of a reinforcement body (3) made of a fibre-reinforced plastics material in such a manner that the reinforcement body (3) arranged on the die core (2) surrounds the die core (2) in a peripheral direction of the die core (2) around a working movement axis (5) of the die core (2), along which working movement axis a workpiece receiving member (4) of the die core (2) extends inside the die core (2), wherein the reinforcement body (3) comprises a plastics matrix and a reinforcing fibre structure (9) which is embedded in the plastics matrix and which extends in the peripheral direction of the die core (2) wherein the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2) such that the core reinforcement which is arranged on the die core (2) is radially pretensioned transversely to the working movement axis (5) against the die core (2), and wherein the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2)• by the reinforcement body (3) being produced as a hardened hollow member which has in the interior thereof a core receiving member (7) for the die core (2), wherein the core receiving member (7) of the reinforcement body (3) has a core receiving member axis (8) which extends along the working movement axis (5) of the die core (2) when the die core (2) is in the mounting position, wherein the core receiving member (7) of the reinforcement body (3) has along the core receiving member axis (8) a core receiving member opening (11) at least at one side and wherein, in an initial assembly state of the reinforcement body (3), the core receiving member (7) of the reinforcement body (3) has an initial core receiving member cross-section which extends perpendicularly to the core receiving member axis (8),• by a readiness for assembly of the reinforcement body (3) and the die core (2) being produced and• by the ready-for-assembly reinforcement body (3) and the ready-for-assembly die core (2) being joined, wherein the ready-for-assembly die core (2) is introduced through the core receiving member opening (11) of the ready-for-assembly reinforcement body (3) along the core receiving member axis (8) into the core receiving member (7) of the ready-for-assembly reinforcement body (3) and the reinforcement body (3) is thereby arranged at the outer side of the die core (2),
characterised in that the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2)• by the readiness for assembly of the reinforcement body (3) and the die core (2) being produced by the core receiving member cross-section (QA) of the reinforcement body (3) being increased with respect to the initial core receiving member cross-section, wherein the core receiving member cross-section (QA) of the ready-for-assembly reinforcement body (3) has such dimensions that the core cross-section (QM) of the ready-for-assembly die core (2) is, in the perpendicular projection onto the core receiving member cross-section (QA), within the core receiving member cross-section (QA), and• by, after the reinforcement body (3) and the die core (2) have been joined so as to produce the radial pretensioning of the reinforcement body (3) against the die core (2), the core receiving member cross-section (QA) of the reinforcement body (3) being decreased. - Method according to claim 2, characterised in that the reinforcement body (3) is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2)• by the core cross-section (QM) of the die core (2) being decreased with respect to a core cross-section for use which is present in a state for use of the die core (2) for producing the readiness for assembly of the reinforcement body (3) and the die core (2), and• by, after the reinforcement body (3) and the die core (2) have been joined so as to produce the radial pretensioning of the reinforcement body (3) against the die core (2), the core receiving member cross-section (QA) of the reinforcement body (3) being decreased and the core cross-section (QM) of the die core (2) being increased.
- Method according to any of the preceding claims, characterised in that the reinforcement body (3) made of fibre-reinforced plastics material is applied directly to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2).
- Method according to at least claim 1 or claim 3, characterised in that the core cross-section (QM) of the die core (2) is decreased with respect to the core cross-section for use by the die core (2) being extended along the working movement axis (5) of the die core (2), preferably resiliently extended, with respect to the state for use.
- Method according to at least claims 1 or claim 3, characterised in that the core cross-section (QM) of the die core (2) is decreased with respect to the core cross-section for use by the temperature of the die core (2) being changed with respect to the temperature in the state for use of the die core (2).
- Method according to at least claim 2 or claim 3, characterised in that the core receiving member cross-section (QA) of the reinforcement body (3) is increased with respect to the initial core receiving member cross-section by the temperature of the reinforcement body (3) being changed with respect to the temperature in the initial assembly state of the reinforcement body (3).
- Method according to any of the preceding claims, characterised in that a reinforcement body (3) made of carbon-fibre-reinforced plastics material is applied to the die core (2) so as to produce a radial pretensioning of the reinforcement body (3) against the die core (2).
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17185483.9A EP3441156B1 (en) | 2017-08-09 | 2017-08-09 | Methods for producing a matrix for pressure forming of workpieces |
CN201810735945.6A CN109383046A (en) | 2017-08-09 | 2018-07-06 | Method for making the shaping dies of workpiece pressure forming and for manufacturing this shaping dies |
US16/048,937 US20190047035A1 (en) | 2017-08-09 | 2018-07-30 | Forming die for pressure-forming workpieces and method for producing a forming die for pressure-forming workpieces |
JP2018149273A JP2019031080A (en) | 2017-08-09 | 2018-08-08 | A forming die for press-molding a workpiece and a method for manufacturing a forming die for pressure-molding a workpiece |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17185483.9A EP3441156B1 (en) | 2017-08-09 | 2017-08-09 | Methods for producing a matrix for pressure forming of workpieces |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3441156A1 EP3441156A1 (en) | 2019-02-13 |
EP3441156B1 true EP3441156B1 (en) | 2019-10-09 |
Family
ID=59626449
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17185483.9A Active EP3441156B1 (en) | 2017-08-09 | 2017-08-09 | Methods for producing a matrix for pressure forming of workpieces |
Country Status (4)
Country | Link |
---|---|
US (1) | US20190047035A1 (en) |
EP (1) | EP3441156B1 (en) |
JP (1) | JP2019031080A (en) |
CN (1) | CN109383046A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102019114438A1 (en) * | 2019-05-29 | 2020-12-03 | Kolibri Metals Gmbh | Forming die with lubrication for pressure forming of metallic workpieces and processes for their production |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2506701A1 (en) * | 1975-02-18 | 1976-08-19 | Eberhard Dipl Ing Wolff | Metal-shaping female die - having outer reinforcements with high E-modulus and low pref. negative thermal expansion coefficient |
GB2199282B (en) * | 1986-12-19 | 1990-01-24 | Honda Motor Co Ltd | Process for producing a urethane moulding |
JPH0741352B2 (en) * | 1992-09-24 | 1995-05-10 | アカマツフォーシス株式会社 | dice |
DE19804700A1 (en) | 1998-02-06 | 1999-08-19 | Danfoss As | Molding tool |
DE19916566B4 (en) * | 1999-04-13 | 2005-07-28 | Wafios Ag | Matrix for highly stressed hollow molds |
DE10101539C2 (en) * | 2001-01-15 | 2003-01-23 | Neumayer Erich Gmbh Co Kg | Process for manufacturing a built shaft |
EP1570976A1 (en) * | 2004-03-04 | 2005-09-07 | Alcan Technology & Management Ltd. | Processes for converting cyclic oligomers into thermoplastic PBT products |
EP2511084B1 (en) * | 2011-04-14 | 2014-11-12 | Magna Steyr Fahrzeugtechnik AG & Co KG | Fibre-reinforced plastic node element and method for producing and using same |
-
2017
- 2017-08-09 EP EP17185483.9A patent/EP3441156B1/en active Active
-
2018
- 2018-07-06 CN CN201810735945.6A patent/CN109383046A/en active Pending
- 2018-07-30 US US16/048,937 patent/US20190047035A1/en not_active Abandoned
- 2018-08-08 JP JP2018149273A patent/JP2019031080A/en active Pending
Non-Patent Citations (1)
Title |
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None * |
Also Published As
Publication number | Publication date |
---|---|
JP2019031080A (en) | 2019-02-28 |
US20190047035A1 (en) | 2019-02-14 |
EP3441156A1 (en) | 2019-02-13 |
CN109383046A (en) | 2019-02-26 |
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